Design objective of high Mach number performance manned flight vehicles is concerned with flight operations such that minimum longitudinal trim drag is achieved; utilization of longitudinal statically unstable vehicles as means of obtaining objective; taking delta wing canard controlled aircraft as example, control concept presented is based on 3 systems of compensating for static instability, mechanical stability augmentation system, autopilot and fuel transfer system; each system is capable of permitting adequate control of aircraft.


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    Title :

    Approach to control of statically unstable manned flight vehicles


    Additional title:

    AGARD -- Report


    Contributors:
    Dublin, M. (author)

    Published in:

    Publication date :

    1961


    Size :

    25 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :




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